This disclosure relates to methods and devices for detecting configurations of aircraft. A sound is recorded from an interior of an aircraft. A transform is calculated of the sound. The transform is compared with a calibration transform of a known configuration. A closeness parameter is determined based on the comparison. A detected configuration is indicated if the closeness parameter is above a threshold.


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    Title :

    Situational Awareness Trainer


    Contributors:
    MOORE RUDY (author)

    Publication date :

    2021-02-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / G09B Unterrichts- oder Vorführungsgeräte , EDUCATIONAL OR DEMONSTRATION APPLIANCES



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